US4387764A - Gasket screening assembly for an internal combustion engine having an auxiliary oil cooler - Google Patents
Gasket screening assembly for an internal combustion engine having an auxiliary oil cooler Download PDFInfo
- Publication number
- US4387764A US4387764A US06/327,259 US32725981A US4387764A US 4387764 A US4387764 A US 4387764A US 32725981 A US32725981 A US 32725981A US 4387764 A US4387764 A US 4387764A
- Authority
- US
- United States
- Prior art keywords
- gasket
- perforations
- assembly
- clear
- oil cooler
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D7/00—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D7/16—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged in parallel spaced relation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/02—Sealings between relatively-stationary surfaces
- F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
- F16J15/10—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing
- F16J15/12—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing with metal reinforcement or covering
- F16J15/121—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing with metal reinforcement or covering with metal reinforcement
- F16J15/122—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing with metal reinforcement or covering with metal reinforcement generally parallel to the surfaces
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F19/00—Preventing the formation of deposits or corrosion, e.g. by using filters or scrapers
- F28F19/01—Preventing the formation of deposits or corrosion, e.g. by using filters or scrapers by using means for separating solid materials from heat-exchange fluids, e.g. filters
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M11/00—Component parts, details or accessories, not provided for in, or of interest apart from, groups F01M1/00 - F01M9/00
- F01M11/03—Mounting or connecting of lubricant purifying means relative to the machine or engine; Details of lubricant purifying means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M1/00—Pressure lubrication
- F01M1/10—Lubricating systems characterised by the provision therein of lubricant venting or purifying means, e.g. of filters
- F01M2001/1007—Lubricating systems characterised by the provision therein of lubricant venting or purifying means, e.g. of filters characterised by the purification means combined with other functions
- F01M2001/1014—Lubricating systems characterised by the provision therein of lubricant venting or purifying means, e.g. of filters characterised by the purification means combined with other functions comprising supply of additives
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M5/00—Heating, cooling, or controlling temperature of lubricant; Lubrication means facilitating engine starting
- F01M5/002—Cooling
Definitions
- Auxiliary oil coolers for internal combustion engines frequently utilize a series of tubes through which coolant passes, and over and around which the oil to be cooled passes. Particulate buildup in the tubes tends to result in blocked tubes, reducing the efficiency of the cooler, and sometimes resulting in engine burn out.
- the auxiliary cooler assembly is secured directly or through a supplementary fitting to the engine block with appropriate gaskets interposed between the block and the auxiliary cooler.
- the gaskets provide four flow paths to and from the block, namely an oil exit path, running from the block to the auxiliary cooler, an oil inlet path returning from the cooler to the block, a coolant exit opening running from the block to the auxiliary cooler, and a coolant inlet opening returning coolant to the block.
- Such flow paths and associated openings in the block, auxiliary cooler fittings and interposed gasket are clear-through openings. Particulate material which develops in the engine and radiator is frequently found in the coolant, is entrained therein and therefore passes into the tubes of the auxiliary cooler.
- an improved and successful mechanism for screening and removing particles from coolant moving from an engine block to an auxiliary cooler has been developed.
- a new gasket assembly has been developed which can be used instead of existing gasket assemblies, but which is specially configured to serve not only as a gasket, but also to screen out and hold back particles of predetermined sizes from passing from the block to the auxiliary oil cooler.
- the gasket screening assembly of this invention not only screens particles, but is configured and assembled such that the materials used in making the gasket itself are not likely to become disassociated from the gasket and thereby pass to the oil tubes where they could also serve to block the tubes.
- An improved screening gasket assembly of this invention has an expansive metallic core having a pair of major surfaces, and a compressible facing layer secured to each major surface of the core about the periphery of each the major surface thereby to surround a central core zone of each major surface which is devoid of a facing layer.
- the assembly defines a first clear-through return opening for coolant, a second clear-through oil exit opening, and a third clear-through oil inlet opening, each in the zones of the facing layers for providing flow-paths between an engine block and an auxiliary oil cooler.
- the core central zone defines a multiplicity of closely adjacent, substantially circular perforations for providing a fourth, water inlet path through the central core zone between the engine block and the oil cooler.
- the screening gasket assembly is adapted to be sealingly disposed between the confronting flanges on the engine block and the oil cooler assembly.
- the flanges clampingly and sealingly grip the screening gasket assembly and define bores in line with and in flow communication with the first through third openings, and the perforations, whereby particles in the coolant passing through the multiplicity of perforations are adapted to be screened therefrom against introduction into the cooler, hence against return through the first clear-through coolant return opening.
- the multiplicity of perforations are arranged in a plurality of staggered rows of perforations.
- FIG. 1 is an exploded view of a gasket assembly of this invention juxtaposed with an engine block with which it is adapted for use;
- FIG. 2 is a fragmentary view showing the gasket assembly of this invention disposed between an engine block and a cooler support;
- FIG. 3 shows the cooler support, the auxiliary cooler and the filter assembly with which the gasket assembly of this invention is adapted to be used;
- FIG. 4 is a cross-sectional view taken substantially along lines 4--4 of FIG. 3;
- FIG. 5 is an enlarged fragmentary view of the filter zone of the gasket assembly of FIG. 1.
- FIG. 1 illustrates a filter gasket assembly 10 of this invention.
- Gasket assembly 10 is adapted to be mounted to an engine block 12 at block flange 14, and between flange 14 and a confronting complementary cooler support flange 16 of cooler support 18.
- Block flange 14 defines a plurality of threaded bolt bores 20, an oil exit opening 22, an oil inlet opening 24, a coolant exit opening 26 and a coolant inlet opening 28. Confronting complementary openings are defined in cooler support flange 16. Bolt holes 30 in support 18 are in line with bores 20, thereby to bolt the support to the block, as via bolts 32.
- Support 18 may be a casting which defines curved internal passageways for oil and coolant to be introduced into the cooler assembly and to be returned from the cooler assembly to the block.
- the block coolant exit opening is in communication with the zone of the cooler assembly between the cooler housing 40 and the heat exchange element 42.
- Heat exchange element 42 comprises a plurality of elongate tubes 44 and spiral fin elements 46 which causes the oil to pass over and between the tubes, to pass through the oil filter 48, for subsequent return to the block through oil inlet opening 24.
- Coolant such as water
- filter gasket assembly 10 desirably comprises an expansive flat metallic core 50 which may be made of 304 stainless steel. Core 50 typically may be 0.008 inch thick. A peripheral facing 52 is laminated to each major surface of core 50. Only one facing 52 is shown. The other is a mirror image. Facings 52 are rubber-fiber facings and may desirably be of an asbestos-rubber material, such as asbestos-nitrile rubber, adhesively laminated to the core. Facings 52 are sufficiently compliant and compressible to effect a seal between the confronting flanges 14 and 16, hence to provide an effective seal at the juncture of the block 12 and cooler support 18.
- Gasket assembly 10 defines a plurality of bolt holes 54 corresponding to the bolt bores 20.
- Bolt holes 54 are located in the zone of the facings 52.
- the gasket also defines appropriate bores to allow oil and water to pass therethrough, including an oil exit bore 62, an oil inlet bore 64 and a coolant inlet bore 68.
- Each of these desirably is in the zone of the facings 52, thereby to provide an effective seal between the block flange openings 22, 24 and 28 and the complementary openings in the confronting cooler support flange 16.
- the block coolant exit opening is in communication with a zone Z of the gasket assembly which is defined by the somewhat irregular openings in the facings shown in FIG. 1.
- substantially the core only defines the exit opening in the gasket assembly through which coolant exits from the block.
- the surrounding peripheral facing portions serve then to seal off the remaining openings from zone Z and to prevent leakage from zone Z outwardly therefrom.
- Zone Z is very substantially larger than the area needed to provide the necessary flow of coolant from exit opening 26.
- a series of perforations 66 are provided in zone Z and the surface area of the perforations are more than adequate to accommodate coolant exit flow from the blade into tubes 44.
- zone Z which comprises solely a metallic perforated screen.
- Perforations 66 most preferably are substantially circular in plan view and are closely spaced in staggered rows, such as the nine rows illustrated.
- the array of perforations is disposed in alignment with opening 26 for the spacing of the core 50 from flange face 14 is maximally the thickness of the facing 52 which is insufficient to provide flow without undue increase in frictional resistance to the flow of the coolant.
- perforations 66 are selected to filter out particles P which would tend to produce obstructions individually or collectively in the tubes, on the one hand, and to minimize pressure build-up and plugging of the perforations in zone Z, on the other hand. It has been determined that perforations approximately 5/32" in diameter are most effective, although openings of from about 1/8" to about 3/16" in diameter will also function satisfactorily. Most desirably, the perforations should be substantially circular. Openings which substantially depart from circular, such as those which are elongate, such as rectangular, will have to be reduced in one dimension to the maximum particle size for which passage is permissible. The other dimension perforce would have to be less, and would therefore also tend to increase pressure drop through the filter zone. Further, rectangular openings would tend to foster break-up of particles, in turn causing particles to pass into the tubes.
- a friction-resistant material such as polytetrafluoroethylene
- the coating is provided on both major surfaces of the gasket assembly, both on the central core portion 50 and on the surface of the facings 52.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
- Gasket Seals (AREA)
Abstract
Description
Claims (6)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/327,259 US4387764A (en) | 1981-12-03 | 1981-12-03 | Gasket screening assembly for an internal combustion engine having an auxiliary oil cooler |
MX194781A MX156248A (en) | 1981-12-03 | 1982-10-14 | IMPROVEMENTS TO PACKAGING AND SIEVE ASSEMBLY BETWEEN AN INTERNAL COMBUSTION ENGINE BLOCK AND AN AUXILIARY OIL COOLER |
GB08234425A GB2110775B (en) | 1981-12-03 | 1982-12-02 | A gasket |
BR8206996A BR8206996A (en) | 1981-12-03 | 1982-12-02 | COMBINED SCREENING AND GASKET SET AND SEALING DEVICE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/327,259 US4387764A (en) | 1981-12-03 | 1981-12-03 | Gasket screening assembly for an internal combustion engine having an auxiliary oil cooler |
Publications (1)
Publication Number | Publication Date |
---|---|
US4387764A true US4387764A (en) | 1983-06-14 |
Family
ID=23275801
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US06/327,259 Expired - Fee Related US4387764A (en) | 1981-12-03 | 1981-12-03 | Gasket screening assembly for an internal combustion engine having an auxiliary oil cooler |
Country Status (4)
Country | Link |
---|---|
US (1) | US4387764A (en) |
BR (1) | BR8206996A (en) |
GB (1) | GB2110775B (en) |
MX (1) | MX156248A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4715434A (en) * | 1985-12-19 | 1987-12-29 | Navistar International Transportation Corp. | Fluid treatment pressure vessel with a disposable cartridge and valve therefor |
US4793302A (en) * | 1986-04-19 | 1988-12-27 | Perkins Engines Group Limited | Engine cooling system |
EP0632246A2 (en) * | 1993-07-02 | 1995-01-04 | Sanden Corporation | Heat exchanger |
US5647315A (en) * | 1994-10-07 | 1997-07-15 | Yamaha Hatsudoki Kabushiki Kaisha | Lubricating arrangement for engine |
WO1998010176A1 (en) * | 1996-09-04 | 1998-03-12 | Filterwerk Mann + Hummel Gmbh | Subassembly for an internal combustion engine |
US6105668A (en) * | 1997-09-10 | 2000-08-22 | Behr Gmbh & Co. | Stacking-disk heat exchanger |
US20040173341A1 (en) * | 2002-04-25 | 2004-09-09 | George Moser | Oil cooler and production method |
US20090020300A1 (en) * | 2007-07-17 | 2009-01-22 | Braddock C Kerwin | Air inlet for pneumatic power tool |
US11421578B1 (en) * | 2019-12-20 | 2022-08-23 | Brunswick Corporation | Combination lubricant/filtration device for outboard motors |
Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB189628671A (en) * | 1896-12-15 | 1897-10-23 | Charles Stowe | Improvements in Traps for Waste Pipes and the like. |
US1236100A (en) * | 1917-03-21 | 1917-08-07 | Franklin Gas Turbine Company | Gasket-screen. |
US1361243A (en) * | 1919-12-04 | 1920-12-07 | Amos J Fuson | Gasolene-filter |
US1362028A (en) * | 1920-09-14 | 1920-12-14 | Miller Lorin Otto | Mixer |
US1398063A (en) * | 1919-05-16 | 1921-11-22 | Clifford C Brown | Mixer for gas-engines |
US1558777A (en) * | 1923-04-05 | 1925-10-27 | James H Barrett | Gasket check valve |
US2504683A (en) * | 1947-05-01 | 1950-04-18 | John H Harnley | Grease gun filter attachment |
US2665009A (en) * | 1951-06-30 | 1954-01-05 | Int Harvester Co | Milk strainer with removable baffle and centering device |
US3622008A (en) * | 1969-12-22 | 1971-11-23 | Flexitallic Gasket Co Inc | Compression gasket and screen assembly |
US3830289A (en) * | 1972-05-18 | 1974-08-20 | D Olson | Oil cooler |
US3919089A (en) * | 1972-11-08 | 1975-11-11 | Refacciones Plasticas Y Metali | Self-tightening filter assembly |
US4174699A (en) * | 1977-12-27 | 1979-11-20 | General Motors Corporation | Engine oil processing system |
-
1981
- 1981-12-03 US US06/327,259 patent/US4387764A/en not_active Expired - Fee Related
-
1982
- 1982-10-14 MX MX194781A patent/MX156248A/en unknown
- 1982-12-02 BR BR8206996A patent/BR8206996A/en unknown
- 1982-12-02 GB GB08234425A patent/GB2110775B/en not_active Expired
Patent Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB189628671A (en) * | 1896-12-15 | 1897-10-23 | Charles Stowe | Improvements in Traps for Waste Pipes and the like. |
US1236100A (en) * | 1917-03-21 | 1917-08-07 | Franklin Gas Turbine Company | Gasket-screen. |
US1398063A (en) * | 1919-05-16 | 1921-11-22 | Clifford C Brown | Mixer for gas-engines |
US1361243A (en) * | 1919-12-04 | 1920-12-07 | Amos J Fuson | Gasolene-filter |
US1362028A (en) * | 1920-09-14 | 1920-12-14 | Miller Lorin Otto | Mixer |
US1558777A (en) * | 1923-04-05 | 1925-10-27 | James H Barrett | Gasket check valve |
US2504683A (en) * | 1947-05-01 | 1950-04-18 | John H Harnley | Grease gun filter attachment |
US2665009A (en) * | 1951-06-30 | 1954-01-05 | Int Harvester Co | Milk strainer with removable baffle and centering device |
US3622008A (en) * | 1969-12-22 | 1971-11-23 | Flexitallic Gasket Co Inc | Compression gasket and screen assembly |
US3830289A (en) * | 1972-05-18 | 1974-08-20 | D Olson | Oil cooler |
US3919089A (en) * | 1972-11-08 | 1975-11-11 | Refacciones Plasticas Y Metali | Self-tightening filter assembly |
US4174699A (en) * | 1977-12-27 | 1979-11-20 | General Motors Corporation | Engine oil processing system |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4715434A (en) * | 1985-12-19 | 1987-12-29 | Navistar International Transportation Corp. | Fluid treatment pressure vessel with a disposable cartridge and valve therefor |
US4793302A (en) * | 1986-04-19 | 1988-12-27 | Perkins Engines Group Limited | Engine cooling system |
EP0632246A2 (en) * | 1993-07-02 | 1995-01-04 | Sanden Corporation | Heat exchanger |
EP0632246A3 (en) * | 1993-07-02 | 1995-04-12 | Sanden Corp | Heat exchanger. |
US5647315A (en) * | 1994-10-07 | 1997-07-15 | Yamaha Hatsudoki Kabushiki Kaisha | Lubricating arrangement for engine |
US5809963A (en) * | 1994-10-07 | 1998-09-22 | Yamaha Hatsudoki Kabushiki Kaisha | Lubricating arrangement for engine |
WO1998010176A1 (en) * | 1996-09-04 | 1998-03-12 | Filterwerk Mann + Hummel Gmbh | Subassembly for an internal combustion engine |
US6105668A (en) * | 1997-09-10 | 2000-08-22 | Behr Gmbh & Co. | Stacking-disk heat exchanger |
US20040173341A1 (en) * | 2002-04-25 | 2004-09-09 | George Moser | Oil cooler and production method |
US20090020300A1 (en) * | 2007-07-17 | 2009-01-22 | Braddock C Kerwin | Air inlet for pneumatic power tool |
US8439124B2 (en) | 2007-07-17 | 2013-05-14 | Black & Decker Inc. | Air inlet for pneumatic power tool |
US11421578B1 (en) * | 2019-12-20 | 2022-08-23 | Brunswick Corporation | Combination lubricant/filtration device for outboard motors |
Also Published As
Publication number | Publication date |
---|---|
BR8206996A (en) | 1983-10-11 |
MX156248A (en) | 1988-07-28 |
GB2110775A (en) | 1983-06-22 |
GB2110775B (en) | 1985-10-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: FELT PRODUCTS MFG. CO., A CORP. OF DE. Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:LISTER, MARC D.;REEL/FRAME:003961/0018 Effective date: 19811116 |
|
MAFP | Maintenance fee payment |
Free format text: PAYMENT OF MAINTENANCE FEE, 4TH YEAR, PL 96-517 (ORIGINAL EVENT CODE: M170); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY Year of fee payment: 4 |
|
AS | Assignment |
Owner name: FEL-PRO INCORPORATED, 7450 NORTH MCCORMICK BOULEVA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:FELT PRODUCTS MFG. CO., A CORP. OF DE;REEL/FRAME:004748/0399 Effective date: 19870212 Owner name: FEL-PRO INCORPORATED, ILLINOIS Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:FELT PRODUCTS MFG. CO., A CORP. OF DE;REEL/FRAME:004748/0399 Effective date: 19870212 |
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FEPP | Fee payment procedure |
Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY |
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MAFP | Maintenance fee payment |
Free format text: PAYMENT OF MAINTENANCE FEE, 8TH YEAR, PL 96-517 (ORIGINAL EVENT CODE: M171); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY Year of fee payment: 8 |
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FEPP | Fee payment procedure |
Free format text: MAINTENANCE FEE REMINDER MAILED (ORIGINAL EVENT CODE: REM.); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY |
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LAPS | Lapse for failure to pay maintenance fees | ||
FP | Lapsed due to failure to pay maintenance fee |
Effective date: 19950614 |
|
STCH | Information on status: patent discontinuation |
Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362 |